Airship.



E. H. KELLY, DEWD;

W. D. PHELPS, TEMPORARY ADMINISTRATOR.

AIRSHIP.

APPLICATION FILED DEC. 18, 1909.

Patented Nov. 12, 1912.

3 SHBETSSHEET 1.

[NVENTUR ATTOHNEX W1 TNESSES E. H. KELLY, DECD.

w. 12 PHELPS, Tammany ADMINISTRATOR.

AIRSHIP,

APPLICATION FILED DBO. m, 1909.

TLP@%4:AL@O Patented N0v.12,1912.

3 BHEETSSHEET 2.

WI TNESSES fa. I ATTORNEY E. H. KELLY, DEG D.

W. D. PHELPS, TEMPORAEY ADMINISTRATOB.

AIHSHIP.

APPLICATION FILED DEO.18, 1909.

Patented Nov. 12, 1912.

3 SHEETS8HEET 3.

WITNESSES JNVENTOR M ,5) m

ATTOHNU UN @TE% i EUGENE H. KELLY, 0F BUFFALO, NEW YORK: W. DARWIN PHELPS TEMPORARY ADMINISTRATOR QF SAID KELLY, DECEASED.

MRSHIP.

Specification of Letters Patent.

Application filed December 18, 1909.

Patented Nov. 12, 1912. Serial No. 533,901.

1' '0 all 10/1077), 'it may concern:

Be it known that I, EUGENE H. KELLY, a citizen of the United States of America, residing at Buffalo, county of Erie, State of New York, have invented certain new and useful Improvements in Airships, of which the following is a full, clear, and exact descriptiou.

My invention relates to airships and those of the bi-plane type in particular.

The main object of my invention has bee-n to provide an airship, which, when under flight, shall be entirely automatic in its action and control and one which can also be operated manually if desired.

Some of the other objects are: to provide an airship with rudders which shall be universal in their action, '27. 0., rudders which shall act in any and every direction; also to provide an airship which when ascending shall not require a long flying start.

' Many other merits of my invention will be apparentto those skilled in the art.

In the drawings which form part of this specification like figures of reference indicate corresponding parts in the different views in which:

Figure 1 is general perspective view of my airship. Fig. 2 is a perspective showing the mechanism of the same. Fig. 3 is a sec tional view taken on the center line of one of the pendulum bearings. Fig. l is a sectional view taken on the center line of one of the main bearings and one of the platform bearings. Fig. 5 is a front View of one of-thc platform hangers, Fig. 6 shows a portion of the plano rudder manual operating means. Fig. '3' shows a section of the connection between the plane rudder lever-and the automatic operating means. Fig. is a sectional view taken on the center line of the box rudder bearings and shows one of the ball joints by which the same are supported. y

i (Fig; 1) represents the-square boa shape body of my airship which extends long'i tudinally with the line of flight. Although square box body is shown, obviously the vertical sides of the body may be left 05 if desired. Extending either side of central portion of the top and bottom of the body 1 are horizontal planes and 3 thus making the plan of the general contour or the ship appear like a Maltese'cross. Supports 4- extend from diagonally opposite corners of the body 1', at any suitable number of places and bearing supports are formed at the junction of the supports 4. Diagonal supports 4? and vertical supports 5 brace and holdthe horizontalplanes in their proper positions; Wire stays 6 may be fastened diagonally from one vertical brace to the other to further increase the rigidity of the airship.

Extending longitudinally through the center of the body 1 is the main shaft 7 which is provided preferably With ball bearings supported at the onal supports 4:. A platform 8 may be swung either mediately or immediately from the shaft 7 and comprises a base 9 and two hinged sides 10. The upper end of each hinged side is bifurcated and pivotally mounted upon pins 11 (Figs. 2 and 5). The bearings which support the platform are shown in Fig. 2 in a conventional manner only, a detailed sectional iew of one of the bearings being shown in Fig. 4 where it will be seen that the bearing for the platform is combined with the main shaft bearing.

t, 12 represents a. section of one of the bosses at the junction of the support 1-. 13 is a section of the ring in which are diametrically disposed the pins 11. An annular flanged ball ring 14 extends through the boss 12 and the end 15, which is of smaller diameter, projects for some distance beyond the face of the boss 12. The interior of the larger portion of the ball ring 1% together with the ring 16, which is screwthreaded to the same, form ball cups for the series of balls 17 and 18. A cone ring 19 is secured to the shaft '7 and forms a cone for both series of balls. The ring 16 provides adjustment for this hearing and is locked in position by the lock ring 20. A flanged annular cone ring 531 extends through the ring 13 and is suitably secured thereto.

The cone ring forms a cone for the series of balls 22 and. which are disposed in ball cups formed by the smaller portion of me cup ring it and the ring 2* which is screw-threads 1 onto e end 15 of the cup ring and which provides means for junction of the diagadjusting the last mentioned series of balls. A lock ring 25 also screws on the end 15 of the cup ring 14 and serves to lock the ring 24 in position.

A hearing member 26 (Fig. 2) is rotatably mounted at the exact center of gravity upon the shaft 7. This bearing member is provided with two right angled cylindrical projections 27 and 27 in which the inner ends of the shafts 28 and 28 are disposed. Rotatably supported at the center of the bearing member is a vertical shaft 29 the upper end of which is supported by the bearing 30, this bearing being preferably carried by the stays 31 as shown. To the upper end of this vertical shaft 29 is secured a helicopter screw propeller 32 and near the bottom of the said shaft is disposed a miter gear 33 which meshes with a miter gear 34 secured on the shaft 7. Means are provided preferably, between the miter gear 33 and the shaft 29 whereby the helicopter propeller 32 may be thrown into or out of action at the will of the operator. The miter gear drive shown is only one of the many forms of transmissions which might be employed to drive the helicopter propeller 32.

At some convenient location, preferably in front and near the bearing member 26 is suspended my automatic pendulum 35 by which all the shipsrudders are automatically manipulated. In Fig. 3 is shown a sectional view of the hearing from which the pendulum is suspended. In that figure 36 is an annular cone ring which is secured to the shaft 7 in any suitable way. The cone ring 36 forms the cone for the two series of balls 37 and 38 and surrounding which is the bearing ring 39. This bearing ring is interiorly screw-threaded at each end and has screwed therein rings 40 and 40 the inner faces of which bear against the balls 37 and 38 and provide adjustment therefor. Lock rings 41 and 41 are screw-threaded over the rings 40 and 40 and serve to lock the same in their proper position.

42 (Fig. 2) is the pivotal member of the pendulum which surrounds the bearing ring 39 and is pivotally mounted upon the pivot rods 43 and 43 which extend for considerable distance beyond the pendulum. Suspended from the pivotal member 42 by a rod 44, is a tank 45 which is preferably of a spherical form. The tank 45 may be used for the storage of fuel or water for the engines and a pipe may be attached thereto for draining purposes and when so arranged I prefer to pass the pipes through the slot 47 in the base of the platform. Obviously the tank 45 may be dispensed with as a bob or weight for the pendulum if desired and the rod 46, which extends from the pendulum rod. 44 may be pivotally secured to the base 9 of the platform 8, thus utilizing the platform with its passengers, engine and accessories, as the bob or weight for the pendulum. By this arrangement more platform space is made available. A rod 48 rises vertically from the pivotal member of the pendulum and is of equal length to the rod 44. Passing through the ends of the rods 44 and 48 which are farthest from the pivot member and slidably disposed therein are are rods 49 and 50. The are rod 50 is provided with teeth in its upper side and a ratchet pawl (not shown) is disposed above theseteeth and is operated by means of the handle 51 whereby the arc rod 50 may be set at different relative positions with the pendulum and made to travel therewith, or maybe operatedindependently by manual means.

The shafts 28 and 28 hereinbefore referred to, run centrally between the horizontal planes 2 and 3 and are supported near their outer ends at the junction of the supports 4. Secured to the outer ends ofthe shafts 28 and 28 are plano rudders 52 and 53 respectively.

Near the inner ends of the shafts 28 and 28 and close to the cylindrical projections 27 and 27 of the bearing member 26 are secured in a rigid manner the levers 64 (Figi- 6). -The levers 54 are provided with lugs f sleeves 57 which are secured thereto in a rigid manner and which extend inwardly for a considerable distance. The apertures through the sleeves 57 are preferably'square in conformation and have slidably disposed therein square rods 58. To the inner ends of rods 58 are secured handles 59 and the outer ends are in engagement, with the slotted-ends 60 of the, double-ended bent levers 56.

Rotatably mounted next to the levers 54 upon the shafts 28 and 28 are levers 61 and 61 the hub of each of which (shown in section in Fig. 6) is provided with'an indentation in which the upper end 62 of the lever 56 fits, whereby the shafts 28 and 28 may be locked with the levers 61 and 61 operated independently by manual means.

The arms of the levers 61 and 61 arecylindrical and are of sufiicient length to extend for some distance past the pivot rods- 43 and 43 to which they are connected, a section of such connectors being shown in Fig. 7, where it will be seen that the sleeves 62 and 63 are slidably and rotatably disposed upon the arms of the levers 61 and 61 and the rods 43 and 43 respectively. Two of these sleeves are placed one on the other at right angles and are connected at their center preferably by means of the screwthreaded studs 64 thus providing pivotal connections between the sleeves 62 and 63.

84 represents the hydrocarbon engine messes which furnishes motive power for my air- 1 ship. This engine is mounted on the exact 1 center line upon the base 9 of the platform 8 and is belted from the driving pulley 85 to the pulley87 fixed on the shaft 7 preferably by means of a plurality of belts 86.

Screw propellers 65 and 66 for convenience shown broken off in Fig. 2, are secured near the front and rear of the ship to the shaft 7 and form the main propelling means 1' for my airship. To the two extreme ends of the ship are secured my box rudders 67 and 68 which i are made of any ligh t,-'- tough mate-rial stretched upon frames 69. The connection between one of the shaft ends and one of the rudders 67 and 68 is clearly shown in i Fig. 8 where it will be seen that the end 80 i of the shaft 7 is spherical. and fits into a socket plate which is secured by any suitj l l I able means to the center of the frame 00. Clamping plates 83 and 83 are detachably fastened to the socket plate 82 and serve to keep the spherical end 80 of the shaft in its place.

The diagonal supports of the frame 69: project through the corners of the box rudders 67 and 68 and are provided at their 5 extreme outer ends with pivotal points 90, 90, 90 and90 To each of these points are 1 connected two wires which run to points in a vertical plane at some place along the shaft 7 but inside the propellers and 06- thus points 90, have wires 91 and 91 (011- .j

nected to each, points 90*, have wires 02 and l 92 ,points 90*, have wires 93 and 93 and 4 points 90, have wires. 94 and 9 1. Of these Wires 91 and 92 converge at junction points 95; Wires 92 and 93 at pointg'96; wires 93 i and 94 atpoints 97; wires 91 and 91 at 5 points 98. The junction points 95, 90, 97 and 98 are held intheir proper positions by the wires 99, 99, 99 and 99. 100 and 101 are frames which are placed 1 in a diagonal position'about the shaft 7.; The frame 100 which is at the front end 1 of the ship is provided ateach of its corners 102, 103, 1041 and 105 with traverses, and the frame 101 is also provided at the corners 106, .107 and 108 with trmerses as shown.

To the junction points and 97 at the 4 front end of the ship are secured respectively, wires109 and 110 which are pivotally connected to the ends 103 and 105 of the frame 100 by means of wires 1 1-5 and 146 respectively each pair of which converge at junction points 147 and 14.8 respectively. Connecting the traverse at the end 103 of the frame 100 with the traverse at the end 100-of the frame 101, are 5 wires 111 and 112 and in a like manner; wires 113 and 111 connect the traverses at the ends 105 and 108 of the frames 100 and 101 respectively. livotally connected to the ends 100 and 108 of theframc 101 are wires i ascent.

115 and 116 the other ends of which are secured to the junction points 05 and 97 re' spcctively at the rear end of the ship.

Junction points 96 and 98 at the front end of the ship are connected by Wires 1.17 i and 118 to the traverses 119 and 120 respectively, and these traverses are connected to the traverses on the ends 104 and 102 of the frame 100 by means of Wires 121 and 122: 123 and 12%. Junction point 96 at the rear of the ship is preferably connected diroot to the end 107 of the frame 101 by means of the wire 12:) and junction point 98 is connected to the end 126 of the frame 101 by means of the wire 127, traverse 12S,

wires 12S) and 130, traverse 131 and Wire 1:32.

The traverse at the end 107 of the frame 101 is connected by wires 133 and 134. to the traverse which is pivotally secured to the rear end of the are rod 50. The front end of the arc rod 50 is connected to the end 104 of the frame 100 by means of the wire 130. The end 120 of the frame 101 is connected to the rear end of the arc rod 49 'by means of the wire 137 and the front end of the said are rod is connected by the wire 138 to the end 102 of the frame 100. At caph corner of the frame 100 are provided handles 139, 14-0, 141 and 142 by which the box rudders may be manually operated.

Rockers 113 to which Wheels 144: are rotatably secured, are secured to the base of the ship to suppin't-the same when upon the ground.

llhen it is desired to operate my airship, the arc rod 50 is thrown out of engagement with the pendulum by releasing the handles 51,'and the handle 139 of the frame 100 is then moved forward and, as both rudders 67 and 08 are connected together and to the frame 100 by means hereinbefore mentioned,

the upper part of the rudders will be tipped backward and the lower-part forward, thus steering the ship in an upward direction. The helicopter propeller 32 is thrown into engagementand the engine 84 started,

;; whereupon the ship will make a smooth forward flight and at the same time a rapid Afterthe ship has reached the desired altitude, the helicopter propeller is F thrown out of action and the rudders 07 and 68 manually set so that the ship will pursue generally a horizontal course, whereupon the notched arcrod 50 is engaged with the pendulum, after which all steering in a plane vertical to the line of flight i entirely automatic. All steering in a plane horizontal to the line of flight. is accomplished by simply manipulating the handles 142 or 1 10 forward or backward without any interference with the pendulum.

()wing to the plurality of notches on the arc rod 50 the rudders 07 and 08 may be set and automatically operated by the pendulum so as to cause the ship to gradually ascend or descend as desired.

It. is practically impossible for my airship to overturn. The pendulum which is mounted upon the pivotal pins 43 and 43, always remains perpendicular and therefore the pivotal pins always level. Now should the ship, for any reason, tend to tip to one side it will easily be seen that there will be a relative movement between the pivotal rods 43 and 43 and the arms of the levers 61 and 61 2'. 6., the arms of the levers 61 and 61 actuated by the pivotal rods and 43 respectively, will be revolved, to a de gree equal to the tip of the ship, and in opposite directions. This will cause the plano rudders 52 and 53 to be tilted oppositely and thus restore the equipoise of the shi This balancing is entirely automatic ant sensitive to the least tilting of the ship thus producing a very smooth operating and effective device.

The plano rudders also provide an effective air brake. \Vhen desiring to make a quick stop orin the case of emergency, it is desired to so use the plano rudders, the handles 59 (Fig. 6) are pressed toward each other, which action releasesthe upper ends 62 of the bent levers 56 from the slotsin the levers 61 and 61 whereupon the levers 54 may be revolved free of the said levers 61 and 61 and the. full area of the plano rudders may be presented at right angles to the line of travel and square of wind.

Obviously some modifications of the details herein shown and described may be made without departing from the spirit of my invention and I do not wish to be limited to the exact embodiment herein shown and described.

What I claim is:

1. An airship comprising one or more horizontal planes extending at right angles to the line of flight, a main shaft running centrally across said horizontal planes and parallel to the line of flight, propellers mounted at the front and rear of said shaft, a source of power, rudders at the front and rear of said shaft, and automatic means for governing said rudders.

2. An airship comprising one or more horizontal planes extending at right anglcs to the linc .of flight, a main shaft running centrally across said horizontal planes and parallelto the line of flight, propellers mounted at the front and rear of said shaft,

means for universally mounting said rudders on said shaft, and automatic means for governing said rudders.

3. An airship comprising one or more horizontal planes extending at right angles to the line of flight, a main shaft running entrally across said horizontal planes and parallel to the line of flight, a bearing mem ber rotatably mounted at the center of said main shaft, a vertical shaft supported by said bearing member, a helicopter propeller mounted upon said vertical shaft, propellers mounted upon said main shaft. rudders at the front and rear of said main shaft, and automatic means for governing said rudders.

4. An airship comprising one or more horizontal planes extending at right angles to the line of flight, a mam shaft running centrally across said horizontal planes and parallel to the line of flight, a bearing member rotatably mounted at the center of said main shaft, a vertical shaft supported by said bearing member, a helicopter propeller mounted upon said vertical shaft, screw propellers on said main shaft, a source of power, transverse shafts running parallel with said horizontal planes and rotatably supported by said bearing member, one at each end of said bearing member, planorudders mounted on the outer end of each of said transverse shafts, box rudders, means for universally connecting said box rudders to said main shaft, and means for automatically operating said plano and said box rudders.

5. An airship comprising one or more horizontal planes extending at right angles to the line of flight, a main shaft running centrally across said horizontal planes and parallel to the line of flight, propellers mounted at the front and rear of said shaft, a source of power, box rudders at the front and rear of said main shaft, a pendulum, means for pivotally mounting said pendulum on said main shaft, automatically operated means for connecting said pendulum with said box rudders, and manually oper ated means for connecting said pendulum to said box rudders and independent of said automatic means.

6. An airship comprising one or more horizontal planes extending at right angles to the line of flight, a main shaft running centrally across said horizontal planes and parallel to the line of flight, propellers mounted at the front and rear of said main shaft, a source of power, boat rudders at the front and rear of said shaft, a bearing member rotat-ably mounted at the center of said main shaft, transverse shafts running parallel with said horizontal planes and rotatably mounted in said bearing member, plano rudders at the outer end of each of said transverse shafts, a pendulum pivotally mounted on said main shaft, automati-i cally operated means connecting said pendulum with said plano rudders, manually operated means connecting said pendulum with said plano rudders, box rudders universally mounted on said main shaft, automatically operated means connecting said pendulum with said box rudders, and manually operated means connecting said per, dulum with said box rudders, whereby the ship is entirely automatic in its operation or i we front and rear of said shaft, a bearing member rotatably mounted at the center of said main shaft, aivertical shaft supported by said bearing member, a helicopter pro 'peller mounted upon said vertical shaft,

transverse shafts running parallel with said horizontal planes and rotatably mounted in said bearing member, piano rudders at the outer end of each of said transverse shafts, a pendulum pivotally mounted on said main shaft, automatically operated means con necting said pendulum with said plano rudders, manually operated means connecting said pendulum with said plano rudders, box rudders universally mounted on said main shaft, automaticallyoperated means connecting said pendulum withsaid box rudders,

and manually operated means connecting said pendulum with said box rudders,whcreby the ship is entirely automatic in its operation or may be manually operated when required independent of said automatic operation.

8. An airship comprising one or more horizontal planes extending at right angles to the line of flight, a main shaft running centrally across said horizontal planes and parallel to the line of flight, propellers mounted at the front and rear of said main shaft, a source of power, a-plat-form pivotally mounted beneath said main shaft, box rudders at the front and rear of said main shaft, a bearing member rotatably mounted at the center of said main shaft, transverse shafts running parallel with said horizontal planes and rotatably mounted in said hearing member, plano rudders at the outer end of each of said transverse shafts, a pendulum pivotally mounted on said main shaft, automatically operated means connecting said pendulum with said piano rudders, manually operated means connecting said pendulum with said plane rudders, box rudders universally mounted on said main shaft,

automatically operated means connecting said pendulum with said box rudders, and manually operated means connecting said pendulum with said box rudders, whereby the ship is entirely automatic in its operation or may be manually operated when required independent of said automatic operation.

9. in an airship comprising one or more horizontal planes extending at right angles to the line of flight, a main shaft running centrally across said horizontal planes and parallel to the line of flight, propellers agree 5 mounted at the front and rear of said shaft,

a source of power, box rudders at the front and rear of said main shaft, a platform universally suspended from said main shaft, a pendulum, means for universally mounting said pendulum on said main shaft, means for pivotally connecting the lower end of said pendulum to said platform, automatically operated means for connecting said pendulum with said box rudders, and manually operated means for connecting said pendulum to said box rudders and independent of said automatic means.

10. In an airship comprising two or more horizontal planes extending at right angles to the line of flight, a main shaft running cent-rally across said horizontal planes and parallel to the line of flight, propellers mounted at the front and rear of said main shaft, a source of power, a platform universally mounted beneath said main shaft, box rudders at the front and rear of said main shaft, a bearing member rotatably mounted at the center of said main shaft, transverse shafts runningv parallel with said horizontal planes and rotatably mounted in said bearing member, plano rudders at [the outer end of each ofsaid transverse shafts, a pendulum pivotally mounted on said main shaft, and pivotally secured at its lower end to the said platform, automatically operated means connecting said pendulum witlrsaid plano rudders, manually operated means connecting said pendulum with said plano rudders, box rudders universally mounted on said main shaft, automatically operated means connecting said pendulum with said box rudders, and manually operated means connecting said pendulum with said box rudders, whereby the ship is entirely automatic in its operation or may be manually operated when required independent of said automatic operation.

11. In an airship the combination with a longitudinal box body; of two horizontal planes extending from each side of the center of said body, a main shaft running centrally through said body, propellers mounted upon said shaft at the front and rear of said body, a source of power, rudders at the front and rear of said body and automatic means for governing said rudders.

12. In an airship the combination with a longitudinal box body; of two horizontal planes extending from each side of the center of said body, a main shaft provided at its ends with ball and socket joints and running centrally through said body, propellers rear of said body, a source of power, box rudders mounted on said ball and socket joints at each end of said main shaft and automatic means for governing said rudders,

13. In an airship the combination with a mounted upon said shaft at the front and longitudinal box body; of two horizontal rotatably mounted at the center of said main f said rotatable lever, plano rudders mounted shaft, a vertical shaft supported by said hearing member, a helicopter propeller j mounted upon said vertical shaft, propellers Z mounted upon said main shaft, a source of I power, rudders at the front and rear of said E box body and automatic means for governing said rudders.

14. In an airship the combination with a longitudinal box body; of two horizontal planes extending from each side of the center of said body, a main shaft running centrally through said body, a bearing member rotatably mounted at the center of said main shaft, a vertical shaft supported by? said bearing member, a helicopter propeller mounted upon said vertical shaft, screw propellers, a source of power, transverse shafts rotatably supported by said bearing memher one at each side of said bearing member, plano rudders mounted on the outer ends of said transverse shafts, box rudders mounted in ball and socket joints at each end of said main shaft and automaticineans for operating said plano and box rudders.

15. In an airship the combination with'a longitudinal box body of one or more horizontal planes extending from each side of the center of said body, a main shaft running centrally through said body, a'bearing member rotatably mounted at the center of i said shaft, avertical shaft supported by said bearing member, a helicopter ropeller member, plano rudders mounted on the ilever secured to each of said transverse shafts, a rotatable lever mounted upon outer ends of said transverse shafts, box rudders mounted in ball and socket joints at each end of said main shaft, automatic means for operating said plano and said box rudders, and manual means for operating said plano rudders independent of said automatic means.

16. In an airship the combination with a longitudinal box body; of two horizontal planes extending from each side of the center of said body, a main shaft running centrally through said body, a bearing member rotatably mounted at the center of said main shaft, a vertical shaft supported by said bearing member, a helicopter propeller mounted upon said vertical shaft, propellers mounted upon said main shaft, a source of power, transverse shafts ratatably supported by said bearing member, a rigid lever secured to each of said transverse shafts, a rotatable lever mounted on each of said transverse shafts, a bent lever rotatably mounted on said rigid lever having on the outer ends ofsaid transverse shafts, box rudders universally mounted at each end of said main shaft and automatic means for governing said plano and box rudders. 17. In an airship the combination with a longitudinal box body; of two horizontal planes extending from each side of the center of said body, a main shaft running centrally through said body, a bearing member rotatably mounted at the center of said main shaft, a vertical shaft supported by said bearing member, a helicopter propeller mounted on said vertical shaft, propellers mounted upon said main shaft, a source of power, transverse shafts rotatably supported by said bearing member, a rigid lever secured to each of said transverse shafts, a rotatable lever mounted upon each of said transverse shafts, a bent lever {rotatablly mounted upon said rigid lever and having its upper end engageable with the hub of said rotatable lever means for moving said bent lever into and out of engagement with said rotatable lever, plano rudders mounted on the outer ends of said transverse shafts, box rudders universally mounted at each end of said main shaft and automatic means for operating said plano and box rudders.

18. In an airship the combination with a longitudinal box body; of two horizontal planes extending from each side of the center of said body, a main shaft running centrally through said body, a bearing member rotatably mounted at the center of said main shaft, a vertical shaft supported by said bearing member, a helicopter propeller mounted on said vertical shaft, propellers mounted upon said main shaft, a source of power, transverse shafts rotatably supported by said bearing member, a rigid each of said transverse shafts, a bent lever rotatably mounted upon said rigid lever and having its upper end engageable with the hub of said rotatable member, a lever sleeve secured to the bottom end of each of said ri id levers, a nonrotatable shaft disposed within each of said lever sleeves, one end of each of said nonrotatablc shafts engaging with the lower ends of said bent levers, the other ends being each provided with a handle, plano rudders mounted on the outer'end of said transverse shafts, box rudders universally mounted at each end of said main shaft and automatic means for operating said plano and box rudders.

19. In an airship the combination with a longitudinal box body; of two horizontal 'planes' extending from each side of the center of said body, a main shaft running centrally through said body, a bearing mem- 65 its upper end engageable with the hub of ber rotatably mounted at the center of said 1 nominee I a main shaft, :1 vertical shaft supported by said bearing member, a helicopter propeller mounted on said vertical shaft, propellers mounted on said main shaft, a source of power, transverse shafts rotatably supported by said bearing member, plano rudders mounted upon said transverse shafts, a rotatable lever mounted upon each of said transverse shafts, means for detachably connectsaid rotatable levers to said transverse shafts, a bearing ring rotatably mounted upon said main shaft, pivotal pins diametrically disposed in said bearing ring, a pendulum pivotally mounted upon said pivotal pins, box rudders and means connecting said pendulum with said box rudders whereby the steerage of the ship is made automatic. i

20. in an airship the combination with a longitudinal box body; of one or more horizontal planes extending from each side of the center of said body, a main shaft running centrally through said body, a bearing member rotatably mounted at the center of said main shaft, a vertical shaft supported by said bearing member, a helicopter propeller mounted on said vertical. shz'iit, pr0= pellers mounted on said main shaft, a source of power, a pendulum, means for pivotally mounting said'penduluin on said main shaft, box rudders, and means connecting said pendulum with said box rudders, whereby the stcei'ag'e of the ship is made automatic.

in an airship the combination with a longitudinal box body; of two horizontal planes extending from each side of said said body, a platform pivotally' supported inediately from said main shaft, and ceni'i-ally below said bearing member, a source of power mounted upon said platform, means connecting said source of power to said main shaft, screw propellersmounted on said main shaft, a bearing ring rotatably mounted on said main shat'hpivotal pins disposed diametrically in said bearing ring, a

pendulum pivot-ally mounted upon said pivotal pins, box rudders at each-end of said main shaft; and means connecting said box rudders with said pendulum whereby the steel-age of the ship is made automatic.

22. In an airship the combination with a longitudinal box body; of two horizontal planes extending from each side of said body, a main shaft running centrally through said bbdy, a platform pivotally supported mediately from said main shaft and centrally below said bearing member, a

source of power mounted upon said platform, means connecting said source of power to said main shaft, screw propellers mounted upon said main shaft, :1, vertical shaft, a l elicoptcr-propeller mounted on said vertical shaft, means connecting said vertical shaft with said source of power, a hearing ring rotatably mounted on said main shaft,

pivotal pins disposed diametrically in said 5 bearing ring, a pendulum pivotally mounted upon said pivotal pins, box rudders at 5 automatic.

:lon itudinal box body; of two horizontal 23. In an airship the combination with 21 planes extending from each side of said 2 body,

a main shaft running centrally througl'i said body, a platform pivotally supported mediately, from said shaft, 1nd centrally below said bearing member, a source of power mounted upon said platform, means connecting said source of power to said main shaft, screw propellers mounted on said main shaft, transverse shafts supported by said bearing member, piano rudders mounted on said transverse shafts, a bearing ring rotatably mounted on said main shaft, pivotal pins disposed diametrically in said bearing ring, a pendulum pivotally mounted upon said pivotal pins, means connecting said transverse shafts with said pivotal pins. box rudders at each end of said main shaft and means connecting said box rudders with said pendulum whereby the steerage of the ship is made autoi'natic.

9-1. in an airship the combination with a longitudinal box body, of two horizontal planes extending from each side of said bot a main shaft running centrally ice through said body, a platform pivotally supbody, a main shalt running centrally through ported mediately from said main shaft and centrally below said bearing member, a source of power mounted upon said plat form, means connecting said source of power 105 to said main shaft, screw propellers mounted upon said main shaft, a vertical shaft, a helicopter propeller mounted on said vertical shaft, means connecting said vertical shaft with said source of power, transverse no shaftssupported by said bearing member, plane rudders mounted on said transverse shafts, a bearing ring rotatably mounted on said main shaft, pivotal pins disposed diametrically in said bearing ring, pendulum pivotally mounted upon said pivotal pins, means connecting said transverse shafts with said pivotal pins, box rudders at each end or" said main shaft, and means connecting said box rudders with said pendulum where- 1 by the steerage of the ship is made automatic.

525". In an airship the combination with a longitudinal box body; of one or more horizontal planes extending from each side of 325 said body, a main shaft running centrally 2 through said body, a platform iuiiversallv :supported mediately from said shaftand centrally below said bearing member, a source of power mounted upon said platsaid pivotal pins and having its lower end pivotally secured to said platform, box rudders at each end of said main shaft and means connecting said box rudders with said pendulum whereby the steerage of the ship is made automatic.

26. In an airship the combination with a longitudinal box body; of one or more horizontal planes extending from eachside of said body, a main shaft running centrally through said body, a platform pivotally supported mediately from said main shaft and centrally below said bearing member, a source of power mounted upon said platform, means connecting said source of power to said main shaft, screw propellers mounted upon said mainshaft, a vertical shaft, a helicopter propeller mounted on said vertical shaft, means connecting said vertical shaft with said source of power, a bearing ring rotatably mountedon said main shaft, pivotal pins disposed diametrically on said bearing ring, a pendulum pivotally mounted upon said pivot pins and having its extreme end pivotally secured to said platform, box rudders at each end of said main shaft, and means connecting said box rudders with said pendulum, whereby the steer-age of the ship is made automatic.

27. In an airship the combination with a longitudinal box body; of one or morehori zontal planes extending from each side of said body, a main shaft running centrally through said body, a source of power, means connecting said source of power with-said main shaft, screw propellers mounted on said. main shaft, box rudders, a pendulum, means for pivotally mounting said penduh m on said main shaft, automatically operated' means connecting said pendulum'with said box rudders, and manually operated.

means connecting said pendulum with said rudders and independent of said automatic means. 7 j p 28. In an airship the" combination with a box body; of one or more horizontal planes extending from each side of said body, a

main shaft running centrally through said body, a source of. power, means connecting said source of power with-said main shaft, screw. propellers mounted on said main shaft, box rudders, abearing ring rotatably mounted upon said main shaft, pivotal pins disposed in sai'd' b'earing ring, a pendulum mounted on" said pivotalpins, means connecting said' pendulum with said box 'ru-ddots, and means carried by said pendulum for disconnecting said box rudders from said pendulum, whereby the steerage of the ship is automatically or manually operated.

29. In an airship the combination with a box body; of two horizontal planes extending from each side of said body, a main shaft running centrally through said body, a source of power, means connecting said source of power with vsaid main shaft, screw propellers mounted on said main shaft, box rudders, a bearing ring rotatably mounted upon said main shaft, pivotal pins disposed in said bearing ring, a pendulum mounted on said pivotal pins,'a-rc rods slidably disposed in said pendulum, means for engageably connecting one of said are rods with said pendulum and means connecting said are rods with said box rudders whereby the steer-age of the ship is made automatic.

30. In an airship the combination with a longitudinal box body; of two horizontal planes extending from each side of said body, a main shaft running centrally through said body, a platform pivotally supported mediately from said main shaft, a source of power, said source of power being mounted upon said platform, means connecting said source of power with said main shaft, screw propellers mounted upon said main shaft, box rudders, a bearing ring rotatably mounted upon saidmain shaft, pivotal pins disposed in said bearing ring, a pendulum mounted on said pivotal pins, are rods slidably disposed in said pendulum, means for engageably connectin one of said are rods with said pendulum ant means connecting said are rods with said box rudders whereby the steer-age of the ship is made automatic.

31. In an airshi longitudinal box b planes extending ody; of two horizontal from each side of said the combination with a body, a main shaft running centrally through said body, a platform pivotally supported mediately from said main shaft, a source of power, said source of power being mounted upon said platform, means connecting said source of power with said main shaft, screw propellers mounted upon said main shaft, box rudders, a bearing ring rotatably mounted upon said main shaft,

pivotal pins disposed in saidbeariug ring,- a pendulum mounted on said pivotal pins,

transverse shafts, plano rudders secured to the outer ends of said transverse shafts, a rotatable lever mounted upon each of said transverse shafts, means for engageably securing said rotatable levers tosaid transverse shafts, -a sleeve rotatably and slidably mounted upon the arm of each of said rotatable levers, a pivotal pin sleeve rotatably and slidably mounted on each of said pivotal pins, a screw-threaded stud pivotally securing said sleeve and said pivotal pin sleeve, arc rods slidably disposed in said pendulum, means for engageably connecting one of said are rods with said pendulum and means connecting said are rods with said box rudders whereby the steerage of the ship is made automatic.

32. in an airship the combination with a longitudinal box body; of two horizontal pivotal pins disposed in said bearing ring, a

pendulum mounted on said pivotal pins, are rods slidably disposed in said pendulum, means for engageably connecting one of said arc rods with said pendulum, frames disposed around said main shaft, wires connecting said arc rods with said frames,wires con necting said frames and wires connecting said box rudders with said frames whereby the steerage of the ship is made automatic.

33, in an airship the combination with a longitudinal box body; of two horizontal planes extending from each side of said body, a main shaft running centrally through said body, a platform pivotally supported mediately from said main shaft, a source of power, said source of power being mounted upon said platform, means con necting said source of power with said main shaft, screw propellers mounted upon said main shaft, box rudders, a bearing ring rotatably mounted upon said main shaft pivotal pins disposed in said bearing ring, a pendulum mounted on. said pivotal pins, are rods slidably disposed in said pendulum, notches cut in one of said arc rods, means held by said pendulum for detachably engaging said notched arc rods-and means connecting said are rods with said box rudders whereby the steer-age of the ship is made automatic. I

34-. in an airshi the combination with a longitudinal box body; of two horizontal planes extending from each side of said body, a main shaft running centrally through said body, a platform pivotally supported mediately from said main shaft, a source of power, said source of power being mounted upon said platform, a plurality of round belts connecting said source of power with said main shaft, screw propellers, box rudders, a bearing ring rotatably mounted upon said main shaft, pivotal pins disposed in said bearing ring, a pendulum mounted on said pivotal pins, are rods slidably disposed in said pendulum, meansfor engageably connecting one of said are rods with said penduium and means connecting said are rods with said box rudders whereby the steerage of the ship is made automatic.

35. "5; an airship the combination with a longitiu- 2 box body; of two horizontal planes amending from each side of said bod a main shaft running centrally through said body, transverse shaft-s, plano rudders mounted on the outer ends of said transrerse shafts, a platform pivotally supported mediately from said main shaft, a source of power mounted on. said platform, means connecting said source of power with said main shaft, screw propellers, box rudders, a bearing ring rotatably mounted upon said main shaft,pivotal pins disposed in said bearing ring, a pendulum mounted on said pivotal pins, means connecting said pivotal pins to said transverse shafts, arc rods slidably disposed in said pendulum, means for engageably connecting one of said are rods with said pendulum and means connecting said arc rods with said box rudders whereby the steerage of the ship is made automatic.

36. In an airship the combination with a longitudinal box body; of two horizontal planes extending from each side of the center of said body, a main shaft running centrally through said body, transverse shafts running parallel with said horizontal planes, plane rudders mounted on the outer ends of said transverse shafts, a platform pivotally supported mediately from said main shaft, a source of power mounted upon said platform, means connecting said source of power with said main shaft, screw propellers, box rudders, a bearing ring rotatably mounted on said main shaft, pivotal pins disposed in said bearing ring, a ,pendulum mounted on said pivotal pins, means connectiru said transverse shafts with said e pivotal pins, are rodsslidably disposed in said pendulum, means for engageably connecting one of said are rods with said pendulum and means connecting said arc rods with said box rudders whereby the steerage of the ship is made automatic.

3'7. in an airship the combination with a longitudinal box body; of two horizontal planes extending from each side of the center of said body, a main shaft running centrally through said body, transverse shafts running parallel with said horizontal planes, plano rudders mounted on the outer ends of said transverse shafts, a platform pivotally supported mediately from said main shaft, a source of power mounted upon said platform, means connecting said source of power with said main shaft, screw propellers, box rudders, a bearing ring rota-- tably mounted on said main shaft, pivotal pins disposed in said bearing ring, a pendulum mounted on said pivotal pins, means connecting said transverse shafts with said pivotal pins, are rods slidably disposed in said pendulum, means for engageably connecting one of said are rods with said pendulum, frames disposed about said main shaft, wires connecting said arc rods with said frames, wires connecting said frames and wires connecting said box rudders to said frames whereby the steerage of the ship is made automatic.

38. In an airship the combination with a longitudinal box body; of two horizontal planes extending from each side of the center of said body, a main shaft running centrally through said body, transverse shafts running parallel with said horizontal planes, plano rudders mounted on the outer ends of said transverse shafts, a platform pivotally supported mediately from said main shaft, a source of power mounted upon said platform, means connecting said source of power with said main shaft, screw propellers, box rudders, a bearing ring rotatably mounted on said main shaft, pivotal pins disposed in said bearing ring, a pendulum mounted on said pivotal pins, means connecting said transverse shafts with said pivotal pins, a rotatable lever mounted upon each of said transverse shafts, means for .engageably securing said rotatable levers to said transverse shafts, a sleeve rotatably and slidably mounted upon the arm of each of said rotatable levers, a pivotal pin sleeve rotatably and slidably mounted on each of said pivotal pins, a screw-threaded stud pivotally securing each of said first mentioned sleeves to the corresponding pivotal pin sleeve, arc rods slidably disposed in said pendulum, means for engageably connecting esa-ace sourceof power mounted upon said platform, a plurality of round belts connecting said source of power with said main shaft, screw propellers, box rudders, a bearing ring rotatably mounted on said main shaft, pivotal pins disposed in said bearing ring, a pendulum mounted upon said pivotal pins, means connecting said transverse shafts to said pivotal pins, are rods slidably disposed in said pendulum, means for engageably connecting one of said are rods with said pendulum and means connecting said are rods with said box rudders whereby the steerage of the ship is made automatic.

40. The combination with an airship provided with box rudders, transverse shafts, plano rudders mounted on said transverse shafts; of a pendulum, means connecting said, transverse shafts with said pendulum, frames disposed between said box rudders and said pendulum and means connecting said frames to said box ruddersvand to said pendulum i whereby the steerage of theship is made automatic.

4-1. The combination with an airship provided with box rudders and plano rudders; of a pendulum, are rods slidably disposed in said pendulum, means for engageably securing one of said are rods to said pendulum, frames, means connecting said boxrudders to said frames and means connecting said frames to said are rods whereby the steerage of the ship is made automatic.

42; The combination with'an airship provided with box rudders and plano rudders;

of a pendulum, arc rods slidably disposed in said pendulum, notches-provided in one of said are rods, means disposed in said pendulum for engageably' securing said notches, frames, means connecting said box rudders to said frames and means connecting said frames to said are rods whereby the steerage of the ship is made automatic.

In testimony whereof I have hereunto set my hand in the presence of two witnesses.

EUGENE H. KELLY.

Witnesses:

J. WM. ELLIS, ETHEL A. KELLY. 

